Registered owner
Pa1 208b-0490 LLC
Owner type
LLC
Serial number
208B0490
Year built
1995
Type
Fixed wing single engine
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
November 30, 1995
Certificate issued
September 12, 2026
Expires
September 30, 2033
Mode S code
ACEBBE

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.

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Airworthiness directives that may apply · 47

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1968In forceSuperseded2026
ADs by the year they took effect: 53 ADs
19681
19691
19701
19751
19771
19782
19802
19861
19881
19903
19921
19941
19951
19961
19972
19982
20012
20022
20031
20042
20053
20063
20071
20083
20093
20112
20121
20142
20151
20161
20211
20221
20231
20241
See all 54 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N9310FMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 208B aircraft

FAA incident reports

No FAA accident or incident reports matched to N9310FMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 208B aircraft

Service difficulty reports · 7

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR ENHA202501102181Bolt · brokenLEFT BRAKE CALIPER INOPERATIVE. MECHANICS FOUND THE BRAKE CALIPER GUIDE PIN BROKEN AND THE PIN/CALIPER HAD DAMAGED THE TORQUE PLATE AS WELL AS THE TIRE/WHEEL ASSEMBLY. MECHANICS REPLACED THE CALIPER, TORQUE PLATE AND WHEEL/TIRE ASSEMBLY WITH NEW OR SERVICEABLJan 9, 2025 · N9310F · Cessna 208B · Landing Gear Brake SystemSDR ENHA20230801003Unknown · unknownDURING SCHEDULED INSPECTION PER CESSNA TASK # 57-10-01-250, CRACKS WERE NOTED ON LH&RH ,FWD AND AFT LOWER STRUT FITTINGS.Aug 1, 2023 · N9310F · Cessna 208B · Wing StructureSDR ENHA20230801002Unknown · unknownDURING SCHEDULED INSPECTIONS PER CESSNA TASK 53-10-00-257 ,A CRACK WAS NOTED AT THE HORIZONYAT RH AFT FITTING.Aug 1, 2023 · N9310F · Cessna 208B · Empennage StructureSDR ENHA20230801001Unknown · unknownDURING SCHEDULED INSPECTION PER CESSNA TASK 53-10-00-250 ,A CRACK WAS NOTED AT UPPER CENTER ENGINE MOUNT FITTING.Aug 1, 2023 · N9310F · Cessna 208B · Engine Mount SectionSDR ENHA202107010059Brake · unknownPILOT REPORTED NO RIGHT BRAKE WHILE TURNING ONTO RUNWAY TO LINEUP AND TAKEOFF ON 19R AT PABE. MAINTENANCE INSPECTED BRAKE ASSEMBLY AND FOUND SERVICEABLE, REPLACED BRAKE LININGS FOR BEST PRACTICES.Jun 30, 2021 · N9310F · Cessna 208B · Landing Gear Brake SystemSDR PNSA060804Turbine Blades · failedIN CRUISE AT 9000 FT, PILOT HEARD A LOUD GRINDING NOISE & ENGINE LOST ALL POWER. DECLARED AN EMERGENCY, ATTEMPTED ENGINE RESTART, NO SUCCESS. STARTER WAS ENGAGED NG SHOWED NO ROTATION & INSTRUMENT LIGHTS DIMMED. PROP FEATHERED, NORMAL LANDING. PRELIMARY REPAug 15, 2006 · N9310F · Cessna 208B · Engine (Turbine/Turboprop)SDR PNSA050201Piston · dislodgedON LANDING AT KCG BRAKING WAS LOSS ON LT SIDE. AIRCRAFT ROLLED OUT NORMAL. MAINTENANCE FOUND TWO BRAKE PISTON SEALS ON LT BRAKE CALIPER HAD FAILED CAUSING A LOSS OF FLUID. CALIPER WAS REPLACED AND BRAKES BLED.Feb 21, 2005 · N9310F · Cessna 208B · Master Cylinder/Brake Valve

STCs that may be installed · 357

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 357 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N9310F before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.